Sélection de la langue

Search

Sommaire du brevet 2836727 

Énoncé de désistement de responsabilité concernant l'information provenant de tiers

Une partie des informations de ce site Web a été fournie par des sources externes. Le gouvernement du Canada n'assume aucune responsabilité concernant la précision, l'actualité ou la fiabilité des informations fournies par les sources externes. Les utilisateurs qui désirent employer cette information devraient consulter directement la source des informations. Le contenu fourni par les sources externes n'est pas assujetti aux exigences sur les langues officielles, la protection des renseignements personnels et l'accessibilité.

Disponibilité de l'Abrégé et des Revendications

L'apparition de différences dans le texte et l'image des Revendications et de l'Abrégé dépend du moment auquel le document est publié. Les textes des Revendications et de l'Abrégé sont affichés :

  • lorsque la demande peut être examinée par le public;
  • lorsque le brevet est émis (délivrance).
(12) Brevet: (11) CA 2836727
(54) Titre français: SYSTEME ET PROCEDE POUR UN JOINT D'INGENIERIE
(54) Titre anglais: SYSTEM AND METHOD FOR AN ENGINEERED JOINT
Statut: Périmé et au-delà du délai pour l’annulation
Données bibliographiques
(51) Classification internationale des brevets (CIB):
  • F16C 11/04 (2006.01)
  • E02B 03/04 (2006.01)
  • F16B 05/00 (2006.01)
  • F16C 11/12 (2006.01)
  • F16G 03/02 (2006.01)
(72) Inventeurs :
  • BUTTERFIELD, DONAL (Etats-Unis d'Amérique)
(73) Titulaires :
  • DONAL BUTTERFIELD
(71) Demandeurs :
  • DONAL BUTTERFIELD (Etats-Unis d'Amérique)
(74) Agent: GOWLING WLG (CANADA) LLP
(74) Co-agent:
(45) Délivré: 2016-08-23
(22) Date de dépôt: 2013-12-16
(41) Mise à la disponibilité du public: 2014-11-20
Requête d'examen: 2015-12-30
Licence disponible: S.O.
Cédé au domaine public: S.O.
(25) Langue des documents déposés: Anglais

Traité de coopération en matière de brevets (PCT): Non

(30) Données de priorité de la demande:
Numéro de la demande Pays / territoire Date
13/898,387 (Etats-Unis d'Amérique) 2013-05-20
14/086,953 (Etats-Unis d'Amérique) 2013-11-21

Abrégés

Abrégé français

Un système et un procédé pour un joint dingénierie selon un mode de réalisation illustratif comprennent un axe de charnière et des boucles qui sétendent à partir des membranes autour de laxe de charnière. De multiples modes de réalisation comprennent des boucles qui sétendent dune membrane supérieure du module et transversale pour se fixer à une seconde membrane supérieure du module et des boucles qui sétendent dune première membrane inférieure du module et transversalement pour se fixer à une seconde membrane inférieure du module.


Abrégé anglais

A system and method for an engineered joint according to one example embodiment includes a hinge pin and loops that extend from membranes around the hinge pin. Multiple embodiments include loops that extend from an upper module membrane and cross to attach to a second upper module membrane and loops that extend from a first lower module membrane and cross to attach to a second lower module membrane.

Revendications

Note : Les revendications sont présentées dans la langue officielle dans laquelle elles ont été soumises.


What is claimed is:
1. A system for an engineered joint, comprising:
an upper module having a first upper module membrane and a second upper module
membrane;
a lower module having a first lower module membrane and a second lower module
membrane;
a hinge pin; and
a plurality of loops extending around the hinge pin, wherein a first loop
extends from the
first upper module membrane around the hinge pin and crosses over itself to
attach to the
second upper module membrane, wherein a second loop extends from the first
lower
module membrane around the hinge pin and crosses over itself to attach to the
second
lower module membrane and wherein each of the loops has a pair of cooperating
slots
extending substantially parallel to the axis of the hinge pin and crosses over
itself and
connects to itself at the slots.
2. The system of claim 1, wherein a vertical force exerted on the
engineered joint is
distributed as vertical and horizontal force components on the loops to pull
the first and second
upper module membranes together and to pull the first and second lower module
membranes
together.
3. The system of claim 1, wherein the engineered joint is a flexible
connection in a flexible
structure to assist the flexible structure in yielding to waves, currents and
impact loads.
4. The system of claim 1, further comprising an upper foamed core
positioned between the
first and second upper module membranes and a lower foamed core positioned
between the first
and second lower module membranes.
5. The system of claim 1, wherein each of the loops extends substantially
perpendicular to
an edge of the membrane from which it extends.

6. The system of claim 1, wherein each of the loops has a length
perpendicular to the axis of
the hinge pin and wherein the length of the loops is substantially equal to
the circumference of
the hinge pin.
7. The system of claim 1, further comprising a reinforcing membrane
positioned over at
least two of the slots.
8. The system of claim 1, wherein the second loop extends around the hinge
pin adjacent to
the first loop.
9. The system of claim 1, wherein the first loop is attached to the second
upper module
membrane and the second loop is attached to the second lower module membrane
using an
adhesive that cures to a solid form of the same material as the membranes.
10. The system of claim 1, further comprising a tab portion extending from
each of the loops.
11. A system for an engineered joint, comprising:
an upper module having a first upper module membrane and a second upper module
membrane;
a lower module having a first lower module membrane and a second lower module
membrane;
a hinge pin; and
a plurality of loops extending around the hinge pin, each of the loops having
a pair of
cooperating slots extending substantially parallel to the axis of the hinge
pin, wherein a
first loop extends from the first upper module membrane around the hinge pin
and
crosses over itself to attach to the second upper module membrane and hooks to
itself at
the slots and wherein a second loop extends from the first lower module
membrane
around the hinge pin and crosses over itself to attach to the second lower
module
membrane and hooks to itself at the slots.
12. The system of claim 11, wherein a vertical force exerted on the
engineered joint is
distributed as vertical and horizontal force components on the loops to pull
the first and second
11

upper module membranes together and to pull the first and second lower module
membranes
together.
13. The system of claim 11, wherein the engineered joint is a flexible
connection in a flexible
structure to assist the flexible structure in yielding to waves, currents and
impact loads.
14. The system of claim 11, further comprising an upper foamed core
positioned between the
first and second upper module membranes and a lower foamed core positioned
between the first
and second lower module membranes.
15. The system of claim 11, wherein each of the loops extends substantially
perpendicular to
an edge of the membrane from which it extends.
16. The system of claim 11, wherein each of the loops has a length
perpendicular to the axis
of the hinge pin and wherein the length of the loops is substantially equal to
the circumference of
the hinge pin.
17. The system of claim 11, further comprising a reinforcing membrane
positioned over at
least two of the slots.
18. The system of claim 11, wherein the second loop extends around the
hinge pin adjacent
to the first loop.
19. The system of claim 11, wherein the first loop is attached to the
second upper module
membrane and the second loop is attached to the second lower module membrane
using an
adhesive that cures to a solid form of the same material as the membranes.
20. The system of claim 11, further comprising a tab portion extending from
each of the
loops.
12

Description

Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.


CA 02836727 2015-12-30
SYSTEM AND METHOD FOR AN ENGINEERED JOINT
[00011
BACKGROUND
[0002] The present invention relates to systems and methods for engineered
joints of
flexible structures.
BRIEF DESCRIPTION OF THE DRAWINGS
[0003] Features and advantages of the various embodiments, and the
manner of attaining
them, will become more apparent and will be better understood by reference to
the
accompanying drawings.
[0004] Figure la is a cross-section view along the line A-A in Figure
lb, and Figure lb is
a side elevation view of an engineered joint of a flexible structure according
to multiple
embodiments and alternatives;
[0005] Figure 2 is a top plan view of loops of the engineered joint
according to multiple
embodiments and alternatives;
[0006] Figure 3 is a front elevation view of a flexible structure with
the engineered joint
according to multiple embodiments and alternatives;
[0007] Figure 4 is a cross-section view of an engineered joint of a
flexible structure
according to multiple embodiments and alternatives;
1

i
CA 02836727 2013-12-16
. = .
Attorney Docket No. 115868.143211cip
[0008] Figure 5 is a side elevation view of the engineered joint
according to multiple
embodiments and alternatives;
[0009] Figure 6 is a top plan view of a loop of the engineered joint
according to multiple
embodiments and alternatives;
[0010] Figure 7 is a perspective view of a reinforcing membrane of the
engineered joint
according to multiple embodiments and alternatives; and
[0011] Figure 8 is a perspective view of a loop of the engineered
joint according to
multiple embodiments and alternatives.
DETAILED DESCRIPTION
[0012] The following description and drawings illustrate embodiments
sufficiently to
enable those skilled in the art to practice the present invention. It is to be
understood that the
disclosure is not limited to the details of construction and the arrangement
of components set
forth in the following description or illustrated in the drawings. The
invention is capable of other
embodiments and of being practiced or of being carried out in various ways.
For example, other
embodiments may incorporate structural, chronological, electrical, process,
and other changes.
Examples merely typify possible variations. Individual components and
functions are optional
unless explicitly required, and the sequence of operations may vary. Portions
and features of
some embodiments may be included in or substituted for those of others. The
scope of the
application encompasses the appended claims and all available equivalents. The
following
description is, therefore, not to be taken in a limited sense.
[0013] Also, it is to be understood that the phraseology and
terminology used herein is
for the purpose of description and should not be regarded as limiting. The use
of "including,"
"comprising," or "having" and variations thereof herein is meant to encompass
the items listed
thereafter and equivalents thereof as well as additional items. Unless limited
otherwise, the
terms "connected," "coupled," and "mounted," and variations thereof herein are
used broadly
and encompass direct and indirect connections, couplings, and mountings.
2

CA 02836727 2015-12-30
[0014] Turning now to the drawings, and more particularly to Figures
la, lb, 4 and 5,
example embodiments of an engineered joint 150 of a flexible structure are
illustrated. The joint
150 includes a hinge pin 30 and loops 14. The loops 14 extend from or are
attached to
membranes 12 on modules 20, wrap around the hinge pin 30, and back to the
modules 20
connecting them together. In certain embodiments, the engineered joint may be
used as part of
flexible structures to assist with separating or isolating liquids, such as
those described in U.S.
Patent No. 6,554,534 to Butterfield (entitled "Flexible structure and method
for controlling the
quality of liquids")
[0015] In multiple embodiments, the membranes 12 are resilient
impermeable
membranes, such as those described in U.S. Patent No. 6,554,534 to
Butterfield. In certain
embodiments, the membrane 12 is a vulcanized rubber, such as silicone rubber
reinforced with a
high strength silica filament or other non-corrosive fiber strong enough to
resist tensile forces
without elongating. However, the membrane 12 may consist of any other material
that can be
reinforced with various fibers for specific tensile loads, withstand a variety
of chemicals and
temperature extremes without physical or chemical change and be pigmented or
coated with
various colors, such as polypropylene, polyethylene, rubber, nylon or vinyl,
for example.
[0016] In some embodiments, the membranes 12 may form single layer
square-shaped
modules, such as those described in U.S. Patent No. 6,554,534 to Butterfield.
The modules may
be made and used in triangles, rectangles or any other shape, size or
proportion. For example,
the modules may be square-shaped and have a height of approximately four feet
and a width of
approximately four feet. The modules may be pigmented or coated with any
color, including
reflective finishes. In some embodiments, for example, the membranes may be
white to retard
marine growth.
[0017] In some embodiments, the module 20 consists of a foamed core
22 sandwiched
between two layers of the impermeable membrane 12, such as that described in
U.S. Patent No.
6,554,534 to Butterfield. In such embodiments, the two layers of the
impermeable membrane 12
may be sealed together at the edges of the module 20, with loops 14 at
specific edges, and not at
others. The module 20 may be made and used in triangles, rectangles or any
other shape, size or
proportion. For example, the module 20 may be square-shaped and have a height
of
3

CA 02836727 2013-12-16
=
Attorney Docket No. 115868.143211cip
approximately four feet and a width of approximately four feet. The module may
be pigmented
or coated with any color, including reflective finishes. In some embodiments,
for example, the
membranes may be white to retard marine growth.
[0018] In certain embodiments, the foam core 22 is a polystyrene
block, foamed with a
high volume of air or inert gas for lightness and high resistance to heat
transfer, or insulation
value. However, the core 22 may consist of any other material, either rigid or
flexible, that can
retain its large-celled sealed structure without deteriorating or failing due
to chemical or physical
impact, or the module may have no core 22.
[0019] In some embodiments, the loops 14 are formed continuously from
the same
material as the membrane 12. In other embodiments, the loops 14 may be
attached to the
membrane 12. The loops 14 may be formed from a vulcanized rubber, such as
silicone rubber
reinforced with a high strength silica filament or other non-corrosive fiber
strong enough to resist
tensile forces without elongating. However, the loops 14 may consist of any
other material that
can resist tensile loads, be reinforced with various fibers for specific
strength, withstand a variety
of chemicals and temperature extremes without physical or chemical change and
be pigmented
or coated with various colors, such as polypropylene, polyethylene, rubber,
nylon or vinyl, for
example. In some embodiments, the loops 14 may be attached to the membranes 12
using an
adhesive that cures to a solid form of the same material as the membranes. In
certain
embodiments, the adhesive is room temperature vulcanizing (RTV) silicone
rubber. However,
the loops 14 may be attached to the membrane 12 using any other material that
can resist tensile
loads and withstand a variety of chemicals and temperature extremes without
physical or
chemical change, such as polypropylene, polyethylene, rubber, nylon or vinyl,
for example.
[0020] The loops 14 may be made and used in rectangles, squares,
parallelograms or any
other shape, size or proportion. As illustrated in Figure 2, the loops 14 may
be a parallelogram,
and as illustrated in Figure 6, the loops may be a rectangle. In some
embodiments, the loops 14
have a length t perpendicular to an edge 220 of the membrane 12 or
perpendicular to an axis of
rotation of the hinge pin. In certain embodiments, the length t may be
approximately the
circumference of the hinge pin, which may reduce seepage of liquids, for
example, through the
joint 150. In some embodiments, the loops 14 have a width co parallel to the
edge 220 of the
4

CA 02836727 2013-12-16
=
Attorney Docket No. 115868.143211cip
membrane 12. In certain embodiments, the width co may be approximately two
inches, three
inches or five inches.
[0021] In some embodiments, the loops 14 may extend from the membrane
12 of the
module 20 at an angle to a cross-section plane, at line A-A (shown in Figure
lb), of the hinge
pin. In certain embodiments, the width co may be approximately two inches and
the loops 14
may make approximately a fourteen degree angle with the cross-section plane at
line A-A. In
other embodiments, the loops 14 may extend from the membrane 12 of the module
20 parallel to
the cross-section plane at line A-A or substantially perpendicular to the edge
220 of the
membrane 12, for example, in some embodiments with a single layer module or
with a double
o layer of membranes sandwiching a buoyant core. In certain embodiments,
the width o) may be
approximately two inches and the loops 14 may wrap around the hinge pin
parallel to the cross-
section plane at line A-A or substantially perpendicular to the axis of
rotation of the hinge pin 30.
[0022] In some embodiments, a tab portion 240 may extend from the
loops 14. In some
embodiments, the tab portions 240 are formed continuously from the same
material as the loops
14. In other embodiments, the tab portions 240 may be attached to the loops
14. The tab
portions 240 may be formed from a vulcanized rubber, such as silicone rubber
reinforced with a
high strength silica filament or other non-corrosive fiber strong enough to
resist tensile forces
without elongating. However, the tab portions 240 may consist of any other
material that can
resist tensile loads, be reinforced with various fibers for specific strength,
withstand a variety of
chemicals and temperature extremes without physical or chemical change and be
pigmented or
coated with various colors, such as polypropylene, polyethylene, rubber, nylon
or vinyl, for
example. In some embodiments, the tab portions 240 may be attached to the
loops 14 using an
adhesive that cures to a solid form of the same material as the membranes. In
certain
embodiments, the adhesive is room temperature vulcanizing (RTV) silicone
rubber. However,
the tab portions 240 may be attached to the loops 14 using any other material
that can resist
tensile loads and withstand a variety of chemicals and temperature extremes
without physical or
chemical change, such as polypropylene, polyethylene, rubber, nylon or vinyl,
for example.
[0023] The tab portion 240 may be made and used in rectangles,
squares, parallelograms
or any other shape, size or proportion. For example, it may be rectangular and
have a width
5

CA 02836727 2013-12-16
=
Attorney Docket No. 115868.143211cip
approximately two times the width co of the loops 14. In certain embodiments,
the width lir may
be approximately four inches, six inches or ten inches.
[0024] As shown in Figures 6 and 8, the loops 14 may include
apertures 60 positioned at
or near the tab portions 240. In some embodiments, the apertures 60 may be
slits. The apertures
60 may have a width approximately one half of the width co of the loops 14. In
certain
embodiments, the width of the apertures may be one inch and the width of the
loops may be two
inches, the width of the apertures may be one and a half inches and the width
of the loops may be
three inches or the width of the apertures may be two and a half inches and
the width of the loops
may be five inches.
[0025] As illustrated in Figures 4, 5 and 7, the joint 150 may be
reinforced with a
reinforcing membrane 15 positioned over the apertures 60. The reinforcing
membrane 15 may
be formed from a vulcanized rubber, such as silicone rubber reinforced with a
high strength silica
filament or other non-corrosive fiber strong enough to resist tensile forces
without elongating.
However, the reinforcing membrane 15 may consist of any other material that
can resist tensile
loads, be reinforced with various fibers for specific strength, withstand a
variety of chemicals
and temperature extremes without physical or chemical change and be pigmented
or coated with
various colors, such as polypropylene, polyethylene, rubber, nylon or vinyl,
for example. In
some embodiments, the reinforcing membrane 15 may be attached to the loops 14
and the tab
portions 240 using an adhesive that cures to a solid form of the same material
as the membranes.
In certain embodiments, the adhesive is room temperature vulcanizing (RTV)
silicone rubber.
However, the reinforcing membrane 15 may be attached to the loops 14 and the
tab portions 240
using any other material that can resist tensile loads and withstand a variety
of chemicals and
temperature extremes without physical or chemical change, such as
polypropylene, polyethylene,
rubber, nylon or vinyl, for example.
[0026] The reinforcing membrane 15 may be made and used in rectangles,
squares or any
other shape, size or proportion. For example, it may be rectangular and have a
width
approximately equal to the width (1) of the loops 14.
6

CA 02836727 2013-12-16
= =
Attorney Docket No. 115868.143211cip
[0027] Returning to Figures la, lb, 4 and 5, in some embodiments,
the hinge pin 30 is a
buoyant, hollow tube of acrylonitrile butadiene styrene (ABS). However, it may
consist of any
other non-corrosive, resilient and durable material of adequate rigidity,
shearing and bearing
strength, such as rigid nylon or wood. In some embodiments, the hinge pin 30
is slightly less
than four feet in length. In other embodiments, it may be approximately five
or six feet in
length.
[0028] In multiple embodiments, the loops 14 wrap around the hinge
pin 30 to connect
the modules 20, creating a flexible connection that assists flexible
structures in yielding to
waves, currents and impact loads and in converting impact loads into tensile
stresses. In some
embodiments, the loops 14 from an upper module and a lower module wrap around
the hinge pin
30 adjacent to one another. The loops 14 may extend parallel to the cross-
section plane at line
A-A or substantially perpendicular to the axis of rotation of the hinge pin
30. The loops 14 may
also make an angle a with the cross-section plane at line A-A, for example, in
some
embodiments with two layers of membranes. In certain embodiments, the angle a
may be
approximately fourteen degrees.
[0029] As illustrated in Figures la and lb, in some embodiments, the
loops 14 extend
from one layer of membrane 12 to wrap around the hinge pin 30 in a spiral
manner and cross to
attach to the other layer of membrane 12 of the module. In such embodiments,
when a vertical
force is exerted on the modules 20 and joint 150, both vertical and horizontal
force components
are exerted on the loops 14. For example, if a vertical tensile force is
exerted on the modules 20
and joint 150, both vertical and horizontal force components are exerted on
the loops 14, the
horizontal component pulling the two layers of membrane 12 together, reducing
any peeling
action of the tab portions 240 and the membranes 12 and increasing strength
and durability of the
joint 150.
[0030] As shown in Figure lb, in certain embodiments, the loops 14 from an
upper
module and a lower module may wrap around the hinge pin 30 such that the loops
from the
upper and lower modules interweave with or cross one another as they wrap
around the hinge pin
30. Such an arrangement of the loops 14 may further reduce any peeling action
of the tab
portions 240 and the membranes 12 and increase strength and durability of the
joint 150. In
7

CA 02836727 2013-12-16
=
Attorney Docket No. 115868.143211cip
other embodiments, the loops 14 from an upper module and a lower module may
extend around
the hinge pin 30 such that the loops from the upper and lower modules do not
interweave with or
cross one another.
[0031] As illustrated in Figures 4, 5 and 8, in some embodiments, the
loops 14 attach to
one layer of membrane 12, wrap around the hinge pin 30, cross over themselves
and hook
together in apertures 60 and attach to the other layer of membrane 12 of the
module. In such
embodiments, when a vertical force is exerted on the modules 20 and joint 150,
both vertical and
horizontal force components are exerted on the loops 14. By crossing the
loops, the horizontal
component pulls the two layers of membrane 12 together, reduces any peeling
action of the tab
portions 240 and the membranes 12 and increases strength and durability of the
joint 150. In
certain embodiments, the joint 150 may be reinforced with the reinforcing
membrane 15
positioned over the apertures 60. The reinforcing membrane 15 may further
increase strength
and durability of the joint 150.
100321 In multiple embodiments, the loops 14 are attached back to the
membranes 12
after they extend around the hinge pin 30. In some embodiments, the tab
portion 240 is attached
back to the membranes 12. In some embodiments, the loops 14 are attached back
to the
membranes 12 using an adhesive that cures to a solid form of the same material
as the
membranes. In certain embodiments, the adhesive is room temperature
vulcanizing (RTV)
silicone rubber. However, the loops 14 may be attached to the membrane 12
using any other
material that can resist tensile loads and withstand a variety of chemicals
and temperature
extremes without physical or chemical change, such as polypropylene,
polyethylene, rubber,
nylon or vinyl, for example.
[0033] Persons of skill in the art will recognize that the engineered
joint of the present
invention provides features that may be used to good advantage in a variety of
applications. For
example, embodiments of the engineered joint resist chemical deterioration and
marine growth
from long exposure in seawater and so are more durable than materials used in
conventional
concrete and steel structures. Embodiments of the engineered joint also assist
flexible structures
in changing form with tidal motion or flooding, thereby reducing bending
stresses. Thin
membranes that resist only tension stresses are much cheaper than conventional
rigid structures
8

CA 02836727 2015-12-30
that resist bending stresses. In addition, embodiments of the engineered joint
assist flexible
structures in yielding to waves, currents and impact loads, converting them
into tensile stresses
too. Embodiments of the joint also pull layers of membranes together, reduce
any peeling action
of the membranes and increase joint strength and durability.
[0034] As illustrated in Figure 3, embodiments of the engineered joint may
be used as
part of a flexible structure to assist with separating or isolating liquids.
Advantages of flexible
structures with embodiments of the engineered joint include: convenient volume
and mass to
facilitate handling, transportation and floating; simple parts and their
assembly facilitating
installing, removal, repair and replacement by unskilled workers; ease of
dismantling to
io encourage easier government agency approvals for use in near shore
waters than for
conventional rigid structures; anchoring methods that simplify positioning the
structures; greater
economy than conventional structures; inert material that renders it more
durable than
conventional structures; buoyancy and flexibility that simplify stress
patterns and reduce the
material needed to resist them, further lowering the cost compared to rigid
structures; hinges to
avoid fatigue failure caused by repeated reverse bending; reduced seepage so
it cannot affect
liquids on the other side; improved isolation and separation, which improve
filter efficiency by
maintaining a low head on the pump; insulation against heat transfer through
the structures;
hinging methods to allow forms that adapt to varying water depths;
adaptability to modifications
to accommodate site conditions; flexibility that yields to impact and is safe
for people, fish and
boats; surfaces in various colors to absorb or reflect heat or to design
visual effects for various
esthetic or psychological purposes; and control of water (or other liquid)
quality to motivate uses
that would otherwise be unfeasible in polluted or frigid water.
[0035] The foregoing description of several embodiments has been
presented for
purposes of illustration. It is not intended to be exhaustive or to limit the
application to the
precise forms disclosed, and obviously many modifications and variations are
possible in light of
the above teaching. It is understood that the invention may be practiced in
ways other than as
specifically set forth herein without departing from the current teachings.
9

Dessin représentatif
Une figure unique qui représente un dessin illustrant l'invention.
États administratifs

2024-08-01 : Dans le cadre de la transition vers les Brevets de nouvelle génération (BNG), la base de données sur les brevets canadiens (BDBC) contient désormais un Historique d'événement plus détaillé, qui reproduit le Journal des événements de notre nouvelle solution interne.

Veuillez noter que les événements débutant par « Inactive : » se réfèrent à des événements qui ne sont plus utilisés dans notre nouvelle solution interne.

Pour une meilleure compréhension de l'état de la demande ou brevet qui figure sur cette page, la rubrique Mise en garde , et les descriptions de Brevet , Historique d'événement , Taxes périodiques et Historique des paiements devraient être consultées.

Historique d'événement

Description Date
Le délai pour l'annulation est expiré 2021-08-31
Inactive : COVID 19 Mis à jour DDT19/20 fin de période de rétablissement 2021-03-13
Lettre envoyée 2020-12-16
Lettre envoyée 2020-08-31
Inactive : COVID 19 - Délai prolongé 2020-08-19
Inactive : COVID 19 - Délai prolongé 2020-08-06
Inactive : COVID 19 - Délai prolongé 2020-07-16
Inactive : COVID 19 - Délai prolongé 2020-07-02
Inactive : COVID 19 - Délai prolongé 2020-06-10
Lettre envoyée 2019-12-16
Représentant commun nommé 2019-10-30
Représentant commun nommé 2019-10-30
Requête pour le changement d'adresse ou de mode de correspondance reçue 2018-01-10
Accordé par délivrance 2016-08-23
Inactive : Page couverture publiée 2016-08-22
Inactive : Taxe finale reçue 2016-06-21
Préoctroi 2016-06-21
Un avis d'acceptation est envoyé 2016-01-25
Lettre envoyée 2016-01-25
Un avis d'acceptation est envoyé 2016-01-25
Inactive : Approuvée aux fins d'acceptation (AFA) 2016-01-21
Inactive : Q2 réussi 2016-01-21
Modification reçue - modification volontaire 2016-01-12
Lettre envoyée 2016-01-08
Toutes les exigences pour l'examen - jugée conforme 2015-12-30
Requête d'examen reçue 2015-12-30
Avancement de l'examen jugé conforme - PPH 2015-12-30
Avancement de l'examen demandé - PPH 2015-12-30
Modification reçue - modification volontaire 2015-12-30
Exigences pour une requête d'examen - jugée conforme 2015-12-30
Inactive : Page couverture publiée 2014-11-25
Demande publiée (accessible au public) 2014-11-20
Inactive : CIB attribuée 2014-03-04
Inactive : CIB attribuée 2014-01-31
Inactive : CIB en 1re position 2014-01-31
Inactive : CIB attribuée 2014-01-31
Inactive : CIB attribuée 2014-01-31
Inactive : CIB attribuée 2014-01-31
Inactive : Certificat de dépôt - Sans RE (Anglais) 2014-01-10
Demande reçue - nationale ordinaire 2013-12-23
Déclaration du statut de petite entité jugée conforme 2013-12-16
Inactive : Pré-classement 2013-12-16

Historique d'abandonnement

Il n'y a pas d'historique d'abandonnement

Taxes périodiques

Le dernier paiement a été reçu le 2015-12-14

Avis : Si le paiement en totalité n'a pas été reçu au plus tard à la date indiquée, une taxe supplémentaire peut être imposée, soit une des taxes suivantes :

  • taxe de rétablissement ;
  • taxe pour paiement en souffrance ; ou
  • taxe additionnelle pour le renversement d'une péremption réputée.

Les taxes sur les brevets sont ajustées au 1er janvier de chaque année. Les montants ci-dessus sont les montants actuels s'ils sont reçus au plus tard le 31 décembre de l'année en cours.
Veuillez vous référer à la page web des taxes sur les brevets de l'OPIC pour voir tous les montants actuels des taxes.

Historique des taxes

Type de taxes Anniversaire Échéance Date payée
Taxe pour le dépôt - petite 2013-12-16
TM (demande, 2e anniv.) - petite 02 2015-12-16 2015-12-14
Requête d'examen - petite 2015-12-30
Taxe finale - petite 2016-06-21
TM (brevet, 3e anniv.) - petite 2016-12-16 2016-11-21
TM (brevet, 4e anniv.) - petite 2017-12-18 2017-10-02
TM (brevet, 5e anniv.) - petite 2018-12-17 2018-11-29
Titulaires au dossier

Les titulaires actuels et antérieures au dossier sont affichés en ordre alphabétique.

Titulaires actuels au dossier
DONAL BUTTERFIELD
Titulaires antérieures au dossier
S.O.
Les propriétaires antérieurs qui ne figurent pas dans la liste des « Propriétaires au dossier » apparaîtront dans d'autres documents au dossier.
Documents

Pour visionner les fichiers sélectionnés, entrer le code reCAPTCHA :



Pour visualiser une image, cliquer sur un lien dans la colonne description du document (Temporairement non-disponible). Pour télécharger l'image (les images), cliquer l'une ou plusieurs cases à cocher dans la première colonne et ensuite cliquer sur le bouton "Télécharger sélection en format PDF (archive Zip)" ou le bouton "Télécharger sélection (en un fichier PDF fusionné)".

Liste des documents de brevet publiés et non publiés sur la BDBC .

Si vous avez des difficultés à accéder au contenu, veuillez communiquer avec le Centre de services à la clientèle au 1-866-997-1936, ou envoyer un courriel au Centre de service à la clientèle de l'OPIC.

({010=Tous les documents, 020=Au moment du dépôt, 030=Au moment de la mise à la disponibilité du public, 040=À la délivrance, 050=Examen, 060=Correspondance reçue, 070=Divers, 080=Correspondance envoyée, 090=Paiement})


Description du
Document 
Date
(aaaa-mm-jj) 
Nombre de pages   Taille de l'image (Ko) 
Dessin représentatif 2014-10-29 1 7
Description 2013-12-15 9 511
Revendications 2013-12-15 4 145
Dessins 2013-12-15 9 73
Abrégé 2013-12-15 1 12
Description 2015-12-29 9 498
Revendications 2015-12-29 3 114
Revendications 2016-01-11 3 110
Dessin représentatif 2016-07-19 1 5
Certificat de dépôt (anglais) 2014-01-09 1 157
Rappel de taxe de maintien due 2015-08-17 1 111
Accusé de réception de la requête d'examen 2016-01-07 1 176
Avis du commissaire - Demande jugée acceptable 2016-01-24 1 160
Avis du commissaire - Non-paiement de la taxe pour le maintien en état des droits conférés par un brevet 2020-01-26 1 541
Courtoisie - Brevet réputé périmé 2020-09-20 1 551
Avis du commissaire - Non-paiement de la taxe pour le maintien en état des droits conférés par un brevet 2021-02-02 1 545
Modification 2015-12-29 8 302
Requête ATDB (PPH) 2015-12-29 4 189
Requête d'examen 2015-12-29 2 46
Modification 2016-01-11 5 150
Taxe finale 2016-06-20 2 45